Propellant requirements for military, commercial and research rocket; how to make usable propellants that do not meet freezing point requirements by use of additives such as ammonium thiocyanate added to hydrazine or water to hydrogen peroxide; nontoxic requirements; size of combustion chamber and injection arrangement; high thermal stability; approximate qualities of some of today's propellants.


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    Title :

    Liquid propellants for manned rocket aircraft


    Additional title:

    Missiles Rockets


    Contributors:

    Published in:

    Publication date :

    1957


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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